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Comments on settling chamber design for quiet, blowdown wind tunnelsTransfer of an existing continous circuit supersonic wind tunnel to Langley and its operation there as a blowdown tunnel is planned. Flow disturbance requirements in the supply section and methods for reducing the high level broad band acoustic disturbances present in typical blowdown tunnels are reviewed. Based on recent data and the analysis of two blowdown facilities at Langley, methods for reducing the total turbulence levels in the settling chamber, including both acoustic and vorticity modes, to less than one percent are recommended. The pertinent design details of the damping screens and honeycomb and the recommended minimum pressure drop across the porous components providing the required two orders of magnitude attenuation of acoustic noise levels are given. A suggestion for the support structure of these high pressure drop porous components is offered.
Document ID
19810011557
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Beckwith, I. E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1981
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-81948
Report Number: NASA-TM-81948
Accession Number
81N20085
Funding Number(s)
PROJECT: RTOP 505-31-23-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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